JPH09501213A - ガスタービンの燃料圧スタート方法 - Google Patents

ガスタービンの燃料圧スタート方法

Info

Publication number
JPH09501213A
JPH09501213A JP7503378A JP50337894A JPH09501213A JP H09501213 A JPH09501213 A JP H09501213A JP 7503378 A JP7503378 A JP 7503378A JP 50337894 A JP50337894 A JP 50337894A JP H09501213 A JPH09501213 A JP H09501213A
Authority
JP
Japan
Prior art keywords
fuel
orifice
psi
manifold
pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP7503378A
Other languages
English (en)
Japanese (ja)
Inventor
チュエン チャン，ヒング
Original Assignee
プラット アンド ホイットニー カナダ，インコーポレイテッド
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by プラット アンド ホイットニー カナダ，インコーポレイテッド filed Critical プラット アンド ホイットニー カナダ，インコーポレイテッド
Publication of JPH09501213A publication Critical patent/JPH09501213A/ja
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F02C9/34—Joint control of separate flows to main and auxiliary burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Control Of Turbines (AREA)
  • Monitoring And Testing Of Transmission In General (AREA)
  • Mobile Radio Communication Systems (AREA)
JP7503378A 1993-06-30 1994-05-25 ガスタービンの燃料圧スタート方法 Pending JPH09501213A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US08/085,514 1993-06-30
US08/085,514 US5329759A (en) 1993-06-30 1993-06-30 Method for regulating fuel flow in a gas turbine engine
PCT/IB1994/000150 WO1995001501A1 (fr) 1993-06-30 1994-05-25 Programme de mise en marche des regimes de pression de carburant dans une turbine a gaz

Publications (1)

Publication Number Publication Date
JPH09501213A true JPH09501213A (ja) 1997-02-04

Family

ID=22192116

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7503378A Pending JPH09501213A (ja) 1993-06-30 1994-05-25 ガスタービンの燃料圧スタート方法

Country Status (5)

Country Link
US (1) US5329759A (fr)
EP (1) EP0705384B1 (fr)
JP (1) JPH09501213A (fr)
DE (1) DE69407790T2 (fr)
WO (1) WO1995001501A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008129652A1 (fr) * 2007-04-06 2008-10-30 Hitachi, Ltd. Appareil de génération de puissance à turbine à gaz et son procédé de démarrage

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100673265B1 (ko) 2000-10-04 2007-01-22 엘지.필립스 엘시디 주식회사 액정표시장치
US6526741B2 (en) * 2000-12-18 2003-03-04 General Electric Company Method and apparatus for removing alkali metal contamination from gas turbine liquid fuels
KR100628261B1 (ko) 2001-04-25 2006-09-27 엘지.필립스 엘시디 주식회사 폴리페닐렌프탈아미드계 물질로 이루어진 배향막을 구비한액정표시소자 및 그 제조방법
EP1278014B1 (fr) * 2001-07-18 2007-01-24 Rolls-Royce PLC Dispositif d'alimentation en carburant
US8820087B2 (en) * 2008-09-08 2014-09-02 Siemens Energy, Inc. Method and system for controlling fuel to a dual stage nozzle
US8056343B2 (en) * 2008-10-01 2011-11-15 General Electric Company Off center combustor liner
US8590310B2 (en) 2012-03-27 2013-11-26 Hamilton Sundstrand Corporation Passive equilization flow divider valve
US20160169120A1 (en) * 2014-12-10 2016-06-16 United Technologies Corporation Fuel Schedule for Robust Gas Turbine Engine Transition Between Steady States
US12221926B2 (en) 2022-06-08 2025-02-11 General Electric Company Multi-temperature fuel injectors for a gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4019315A (en) * 1973-06-20 1977-04-26 Westinghouse Electric Corporation Gas turbine power plant control apparatus including a temperature reset starting control system and an ignition pressure control system
US4474014A (en) * 1981-09-17 1984-10-02 United Technologies Corporation Partially unshrouded swirler for combustion chambers
GB2174147B (en) * 1985-04-25 1989-02-01 Rolls Royce Improvements in or relating to the operation of gas turbine engine fuel systems
US4903478A (en) * 1987-06-25 1990-02-27 General Electric Company Dual manifold fuel system
US4817389A (en) * 1987-09-24 1989-04-04 United Technologies Corporation Fuel injection system
US4920740A (en) * 1987-11-23 1990-05-01 Sundstrand Corporation Starting of turbine engines
US5165223A (en) * 1990-12-10 1992-11-24 Sundstrand Corporation Process for starting a gas turbine and gas turbine
US5261222A (en) * 1991-08-12 1993-11-16 General Electric Company Fuel delivery method for dual annular combuster
CA2072275A1 (fr) * 1991-08-12 1993-02-13 Phillip D. Napoli Systeme d'alimentation en carburant pour double chambre annulaire de combustion

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008129652A1 (fr) * 2007-04-06 2008-10-30 Hitachi, Ltd. Appareil de génération de puissance à turbine à gaz et son procédé de démarrage

Also Published As

Publication number Publication date
DE69407790T2 (de) 1998-08-06
EP0705384A1 (fr) 1996-04-10
DE69407790D1 (de) 1998-02-12
US5329759A (en) 1994-07-19
EP0705384B1 (fr) 1998-01-07
WO1995001501A1 (fr) 1995-01-12

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